Ceramic matrix composite turbine vane and method for making

A turbine vane comprising ceramic matrix composite materials. The turbine vane includes an vane support core, an airfoil, and a pair of end walls that are spaced apart from one another to define a gas path. The turbine vane is formed from a plurality of ceramic plies or preforms that are infiltrated...

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Bibliographic Details
Main Authors Shinavski, Robert J, Freeman, Ted J, Tran, Thomas, Brown, Steffan, Lukhard, Kevin
Format Patent
LanguageEnglish
Published 02.11.2021
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Summary:A turbine vane comprising ceramic matrix composite materials. The turbine vane includes an vane support core, an airfoil, and a pair of end walls that are spaced apart from one another to define a gas path. The turbine vane is formed from a plurality of ceramic plies or preforms that are infiltrated with ceramic matrix material to form a one-piece ceramic matrix composite turbine vane.
Bibliography:Application Number: US201916428319